Weapons of Mass Destruction (WMD)
RT-20P / SS-15 SCROOGE
Specifications |
DIA |
|
SS-X-15 (SS-XZ-15) |
NATO |
|
Scrooge |
Bilateral |
|
|
Service |
|
RT-20P RT-20PII - silo version |
OKB/Industry |
|
8K99 (15II696) |
Years of R&D |
|
1965-1969 |
Design Bureau |
|
OKB-586 (Acad. M. K. Yangel) |
Approved |
|
8/24/1965 |
Engineering and Testing |
|
1963-1967/69 |
First Flight Test |
|
10/1967 |
IOC |
|
1969 |
Deployment Date |
|
Not deployed 10/__/1969 |
Type of Warhead |
|
Single |
Warheads |
|
1 |
Yield (Mt) |
|
0.5 or 1.5 |
Payload (t) |
|
0.545 or 1.410 |
Total length (m) |
|
17.48-17.8 |
Total length w/o warhead (m) |
|
16.2 |
Missile Diameter (m) |
|
1.8 |
Launch Weight (t) |
|
30-30.2 |
Fuel Weight (t) |
|
25.4 |
Range (km) |
|
11000 or 7000-8000 |
CEP (m) (Russian Sources) |
|
2000-4000 |
CEP (m) (Western Sources) |
|
600-1800 |
Number of Stages |
|
2 |
Canister length (m) |
|
18.90 |
Canister length w/o front meters (m) |
|
NA |
Canister Diameter (m) |
|
2 |
Booster guidance system |
|
|
|
|
1st stage |
|
2nd stage |
Length (m) |
|
6.12 |
|
8.4 |
Body diameter (m) |
|
1.8 |
|
1.8 |
Fueled weight (t) |
|
16.7 |
|
8.9 |
Dry weight (t) |
|
|
|
|
Liquid Engine Designation |
|
N/A |
|
RD-857 (15D12) (8K94) |
Solid Motor Designation |
|
RDTT 15D15 |
|
N/A |
Design Bureau |
|
|
|
Acad. M. K. Yangel |
Years of R&D |
|
|
|
1963-1967 terminated |
Propellants |
|
Solid |
|
Liquid Storable |
Fuel |
|
N/A |
|
UDMH |
Oxidizer |
|
N/A |
|
AT=AK-27P, N204, Nitrogen Tetrioxide |
Burning time (sec.) |
|
210 + 5 |
|
|
Thrust Sea Level /
Vacuum (Tonnes) |
|
60 |
|
114-115 |
Specific Impulse Sea Level/Vacuum (sec.) |
|
? |
|
329.5 vacuum |
Basing Mode |
|
Ground mobile & silo concept (SLBM?) |
Hardness |
|
|
Launching Technique |
|
Cold |
Deployed Boosters |
|
0 |
Test Boosters |
|
|
Warheads Deployed |
|
0 |
Deployment Sites |
|
|
Training Launchers |
|
|
Space Booster Variant |
|
NA |
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